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King Air 350 – 300 Limitations & Memory Items on V-Speeds, ITT, Fuel, Autopilot & Weight Limits | Aircraft Systems 2026

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This document contains approximately 300 expert-verified limitation questions and answers for the King Air 350 (2026), covering critical V-speeds, engine parameters, fuel system restrictions, autopilot limitations, environmental limits, and aircraft weight and balance constraints. The material provides a comprehensive memory-based review of operational airspeeds including Va, Vfe, Vlo, Vle, Vmca, Vmo, Vx, Vy, Vxse, blue line (Vyse), emergency descent speed, icing minimums, and turbulent air penetration speeds. The document thoroughly addresses engine and propeller limitations including ITT limits (start, idle, takeoff, transient, reverse), torque limits (takeoff, max continuous, cruise climb, transient), N1 limits, prop RPM limits, oil pressure and temperature ranges, generator limits, starter duty cycles, and autofeather requirements. Fuel system limitations are detailed extensively, including approved fuels (Jet A, Jet A-1, Jet B, JP-series), emergency fuel restrictions, usable fuel quantities, crossfeed rules, imbalance limits, standby pump requirements, and fuel pressure limitations. Operational restrictions such as icing procedures, engine anti-ice usage, flap and landing gear limits, yaw damper requirements, rudder boost requirements, brake de-ice limits, steep approach restrictions, and crosswind/tailwind considerations are also covered. Avionics and automation limitations are included in depth, covering autopilot engagement heights, intercept angles, ADC/AHRS requirements, FMS database requirements, RAIM availability, VNAV restrictions, composite mode limitations, and MFD/PFD operational requirements. Structural and performance limits such as maximum ramp weight, takeoff and landing weight, zero fuel weight, baggage and nacelle locker limits, CG aft limit, maximum OAT, cabin differential pressure, and occupancy limits are clearly outlined. The document serves as a structured, exam-focused study tool for aircraft systems oral exams, type ratings, recurrent training, and checkride preparation. This material is particularly relevant for pilots preparing for King Air 350 initial or recurrent training, Part 135 and Part 91K operators, corporate flight department crew members, simulator training candidates, and ATP applicants preparing for turboprop systems evaluations. It aligns closely with the King Air 350 Pilot’s Operating Handbook (POH) / Airplane Flight Manual (AFM) limitations section and manufacturer-approved training curriculum for systems and memory items. Keywords: king air 350 limitations, king air 350 v speeds, maneuvering speed va 184, maximum flap extension speed vfe, vmca flaps up down, vmo 263 0.58 mach, blue line 125, emergency descent speed 184, icing minimum speed 140 kias, torque limits 100 percent 156 transient, ITT limits 820 850 transient, prop rpm limits , oil pressure limits 90 135 psi, usable fuel 539 gallons, fuel crossfeed limitations, generator limits 100 percent 95 percent, autopilot engagement heights 400 agl, FMS RAIM requirements, VNAV limitations, CG aft limit 208 inches

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King Air 350 Limitations 2026
Expert Verified | Ace the Test



Maneuvering Speed Va - 🧠 ANSWER ✔✔184




Do not make full or abrupt control movements above these speeds


Maximum Flap Extension/Extended Speed Vfe - 🧠 ANSWER ✔✔Approach

position 202

Full down position 158

,Do not extend or operate with flaps extended above these speeds.


Maximum landing gear Operating speed Vlo - 🧠 ANSWER ✔✔Extension

184

Retraction 166




Do not extend or retract landing gear above these speeds


Maximum Landing gear extended speed Vle - 🧠 ANSWER ✔✔184


Minimum Control Speed Vmca - 🧠 ANSWER ✔✔Flaps up 94


Flaps down 93




These are the lowest airspeeds at which the airplane is directionally

controllable when one engine suddenly quits, with autofeather armed, and

the other engine at takeoff power.


Maximum Operating Speed - 🧠 ANSWER ✔✔Sea Level to 21,000........263


21,000-35,000...................263-194 (red pointer reflects limits)

Mach speed..................... .58 Mach

, These speeds may not be deliberately exceeded in any flight regime


One Engine inoperative best angle-of-climb Vxse - 🧠 ANSWER ✔✔125


One Engine inoperative best rate of climb (blue line)


Also enroute climb - 🧠 ANSWER ✔✔125


Emergency descent max speed - 🧠 ANSWER ✔✔184


Maximum range glide airspeed - 🧠 ANSWER ✔✔135


Minimum speed KIAS in icing conditions - 🧠 ANSWER ✔✔140 KIAS


Max demonstrated crosswind component - 🧠 ANSWER ✔✔20 knots (this is

not a limit)

Max demonstrated components for coupled approaches - 🧠 ANSWER

✔✔Crosswind.....32 kts


Tailwind...........14 kts


Turbulent air penetration - 🧠 ANSWER ✔✔170 knots


Maximum airspeed for effective windshield anti-icing - 🧠 ANSWER ✔✔226

knots

COPYRIGHT©PROFFKERRYMARTIN 2025/2026. YEAR PUBLISHED 2026. COMPANY REGISTRATION NUMBER: 619652435. TERMS OF USE.
PRIVACY STATEMENT. ALL RIGHTS RESERVED

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